model answer 3

4
Kul-24.3300 Ship Buoyancy and Stability Model Answer 13.10.2012 Assignment 3. Markus Tompuri 1(4) 1. Let us consider metacentric height of the buoy: 0 0 GM The buoy is stable and floats upright 0 0 GM The buoy is unstable and floats inclined Metacentric height of the buoy can be determined with following equation: 2 2 0 0 0 0 H I T KG M B KB GM T Where T is the draft of the buoy, I T is the waterplane moment of inertia and H is the height of the buoy. Lifting force of the buoyancy is equal to the weight of the buoy: g mg Where m is the mass of the buoy and is the water density. 3 3 m 0.020 kg 1000 kg 20 m m Volume of displacement of the buoy is: T D 2 4 Where D is the diameter of the bottom. Thus the draft is: m 0.126 m 0.45 m 0.020 4 4 2 3 2 D T Waterplane area of the buoy is circular, so the moment of inertia can be calculated with following equation: 4 4 4 m 0.002 64 m 0.45 64 D I T When we calculate the GM, we get: m 0.162 2 m 0.65 m 0.020 m 0.002 2 m 0.126 3 4 0 GM 0 0 GM Buoy is unstable and floats inclined.

Upload: av

Post on 02-Oct-2015

3 views

Category:

Documents


0 download

DESCRIPTION

ship stability

TRANSCRIPT

  • Kul-24.3300 Ship Buoyancy and Stability Model Answer 13.10.2012Assignment 3.Markus Tompuri 1(4)

    1. Let us consider metacentric height of the buoy:

    ! 00GM The buoy is stable and floats upright 00GM The buoy is unstable and floats inclined

    Metacentric height of the buoy can be determined with following equation:

    220000HITKGMBKBGM T

    Where T is the draft of the buoy, IT is the waterplane moment of inertia and H is theheight of the buoy. Lifting force of the buoyancy is equal to the weight of the buoy:

    gmg U '

    Where m is the mass of the buoy and U is the water density. 33 m0.020kg1000

    kg20 m

    mU

    Volume of displacement of the buoy is:

    TD 24S

    Where D is the diameter of the bottom. Thus the draft is:

    m0.126m0.45m0.02044

    2

    3

    2

    SSDT

    Waterplane area of the buoy is circular, so the moment of inertia can be calculatedwith following equation:

    444 m0.00264

    m0.4564

    SSDIT

    When we calculate the GM, we get:

    m0.1622

    m0.65m0.020m0.002

    2m0.126

    3

    4

    0 GM

    00GM Buoy is unstable and floats inclined.

  • Kul-24.3300 Ship Buoyancy and Stability Model Answer 13.10.2012Assignment 3.Markus Tompuri 2(4)

    2. If the ship has N number of tanks, the combined free surface effect to themetacenric height can be calculated with following equation:

    jT

    N

    jjtcorr iGMGM ,

    1,0

    1

    UU

    Lets first calcualte the uncorrected metacentric height:

    mmmKGKMGM 0.10.60.700

    We look at three different cases based on the figure below. Length of the tanks isalways lj = 20 m. All the tanks contain ballast water, therefore,

    jmkg

    jt 31025, UU

    Volume of the displacement is:

    33

    9.78041025

    1080002

    mkg

    mkg

    Lets calculate the corrected (effective) metacentric heights for different cases:

    a)

    mm

    mmm

    blGM

    iGMGMN

    jjTcorr

    125.09.780412

    16200.1

    121

    1

    3

    3

    31

    0

    1,0

  • Kul-24.3300 Ship Buoyancy and Stability Model Answer 13.10.2012Assignment 3.Markus Tompuri 3(4)

    b)

    mm

    mmm

    blGM

    iGMGMN

    jjTcorr

    781.09.780412

    82020.1

    1221

    1

    3

    3

    32

    0

    1,0

    c)

    mm

    mmm

    blGM

    iGMGMN

    jjTcorr

    945.09.780412

    42040.1

    1241

    1

    3

    3

    33

    0

    1,0

    3. Ship speed is Vs = 21 kn = 10.8 m/s

    Yaw motion angular velocity:

    rV

    DV s

    s

    s 2

    \

    Centrifugal force acting on the center of gravity of the ship:

    ss

    kp VDF \U\U 2

    2

  • Kul-24.3300 Ship Buoyancy and Stability Model Answer 13.10.2012Assignment 3.Markus Tompuri 4(4)

    Having neglected the rudder forces, for the equilibrium the hydrodynamic reactionand the centrifugal force have the same magnitude.

    The heeling moment is:

    2TKGVM sext \U

    Righting static moment (approximation of initial stability):

    MU sin0GMgM st

    In the equilibrium situation (steady turn) sum of the moments is zero, therefore:

    q

    8.6

    4.081.92

    82.6/8.10

    550/8.10arcsin2arcsin

    2sin

    0sin2

    0

    30

    0

    0

    I

    \I

    \I

    MU\U

    m

    mmsm

    msm

    GMg

    TKGV

    GMg

    TKGV

    GMgTKGV

    MM

    sms

    s

    s

    stext